IT1076144B - Sistema di aumento della stabilita' di un aeromobile - Google Patents

Sistema di aumento della stabilita' di un aeromobile

Info

Publication number
IT1076144B
IT1076144B IT22282/77A IT2228277A IT1076144B IT 1076144 B IT1076144 B IT 1076144B IT 22282/77 A IT22282/77 A IT 22282/77A IT 2228277 A IT2228277 A IT 2228277A IT 1076144 B IT1076144 B IT 1076144B
Authority
IT
Italy
Prior art keywords
increase system
stability increase
aircraft stability
aircraft
stability
Prior art date
Application number
IT22282/77A
Other languages
English (en)
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of IT1076144B publication Critical patent/IT1076144B/it

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
IT22282/77A 1976-04-12 1977-04-08 Sistema di aumento della stabilita' di un aeromobile IT1076144B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/675,707 US4032083A (en) 1976-04-12 1976-04-12 Automatic gain control for stability augmentation systems

Publications (1)

Publication Number Publication Date
IT1076144B true IT1076144B (it) 1985-04-24

Family

ID=24711644

Family Applications (1)

Application Number Title Priority Date Filing Date
IT22282/77A IT1076144B (it) 1976-04-12 1977-04-08 Sistema di aumento della stabilita' di un aeromobile

Country Status (8)

Country Link
US (1) US4032083A (it)
JP (1) JPS52126900A (it)
CA (1) CA1081828A (it)
DE (1) DE2715690A1 (it)
FR (1) FR2348104A1 (it)
GB (1) GB1538968A (it)
IL (1) IL51714A (it)
IT (1) IT1076144B (it)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4115755A (en) * 1976-06-11 1978-09-19 United Technologies Corporation Aerodynamic surface load sensing
US4304375A (en) * 1979-05-17 1981-12-08 Textron Inc. Electrically controlled elevator
US4312042A (en) * 1979-12-12 1982-01-19 Sundstrand Data Control, Inc. Weight, balance, and tire pressure detection systems
US4312039A (en) * 1980-01-24 1982-01-19 Sperry Corporation Transient free synchronization system
US4545019A (en) * 1982-06-18 1985-10-01 Sundstrand Corporation Aircraft in-flight center of gravity measuring system
US5971325A (en) * 1997-12-23 1999-10-26 Sikorsky Aircraft Corporation Compensation for rotorcraft pitch axis control saturation
US7762501B2 (en) * 2005-08-31 2010-07-27 Bell Helicopter Textron Inc. Method and apparatus for improving main rotor yoke fatigue life
US7742846B2 (en) * 2006-06-02 2010-06-22 Sikorsky Aircraft Corporation Surface contact override landing scheme for a FBW rotary-wing aircraft
MX2021007864A (es) * 2016-02-23 2023-01-31 Deka Products Lp Sistema de control de dispositivo de movilidad.

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA624266A (en) * 1961-07-25 Kolisch Emil Center of gravity equipment for aircraft
US3071335A (en) * 1958-10-03 1963-01-01 United Aircraft Corp Flight control system
US3194058A (en) * 1962-09-18 1965-07-13 Kurkjian Haig Weight and balance determination
FR1353123A (fr) * 1963-02-13 1964-02-21 North American Aviation Inc Système de commande de vol automatique pour hélicoptère
US3616691A (en) * 1969-03-26 1971-11-02 Bendix Corp Mission capability indicating system
US3701279A (en) * 1971-02-08 1972-10-31 Electro Dev Corp Aircraft weight and center of gravity indicator system

Also Published As

Publication number Publication date
DE2715690A1 (de) 1977-10-20
GB1538968A (en) 1979-01-24
FR2348104B1 (it) 1982-07-23
US4032083A (en) 1977-06-28
JPS52126900A (en) 1977-10-25
FR2348104A1 (fr) 1977-11-10
CA1081828A (en) 1980-07-15
IL51714A (en) 1981-07-31

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